Updates to the Fokker-120NG
[fg:toms-fgdata.git] / Aircraft / fokker100 / f120ng.xml
1 <?xml version="1.0"?>
2 <?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
3 <fdm_config name="Fokker-100" version="2.0" release="ALPHA"
4    xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
5    xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
6
7  <fileheader>
8   <author> Erik Hofman </author>
9   <filecreationdate> 2010-08-08 </filecreationdate>
10   <version>$Revision: 1.10 $</version>
11   <description> Fokker-100 commercial airliner </description>
12   <reference title="Butterworth-Heinemann - Civil Jet Aircraft Design (BH)
13         http://www.elsevierdirect.com/companions/9780340741528/appendices/data-a/table-8/table.htm"/>
14   <reference title="Lissys - PIANO aircraft analysis software
15         http://www.lissys.demon.co.uk/f7tx2.html"/>
16   <reference title="Aerodynamic Design of Transport Aircraft
17         http://www.scribd.com/doc/23956816/Aerodynamic-Design-of-Transport-Aircraft"/>
18  </fileheader>
19
20 <!--
21   File:     f120ng.xml
22   Inputs:
23     name:          NG-Aircraft F-120NG
24     type:          two-engine transonic transport
25     max weight:    95013.45 lb
26     wing span:     95.03048 ft
27     length:        108.6325 ft
28     wing area:     1025.9045 sq-ft
29     gear type:     tricycle
30     retractable?:  yes
31     # engines:     2
32     engine type:   turbine
33     engine layout: aft fuselage
34     yaw damper?    yes
35
36   Outputs:
37     wing loading:  83.35 lb/sq-ft
38     CL-alpha:      4.4 per radian
39     CL-0:          0.2
40     CL-max:        1.72
41     CD-0:          0.02
42     K:             0.043
43
44 -->
45
46  <metrics>
47    <wingarea  unit="FT2"> 1025.90 </wingarea>
48    <wingspan  unit="FT" >   92.13 </wingspan>
49    <wing_incidence>          2.00 </wing_incidence>
50    <chord     unit="FT" >   12.4671 </chord>
51    <htailarea unit="FT2">  233.792 </htailarea>
52    <htailarm  unit="FT" >   52.4934 </htailarm>
53    <vtailarea unit="FT2">  132.396 </vtailarea>
54    <vtailarm  unit="FT" >   44.6194 </vtailarm>
55    <location name="AERORP" unit="IN">
56      <x> 699.48 </x> <!-- 668.48 -->
57      <y>   0.00 </y>
58      <z>  38.00 </z>
59    </location>
60    <location name="EYEPOINT" unit="IN">
61      <x> 122.04 </x>
62      <y> -30.00 </y>
63      <z>  88.94 </z>
64    </location>
65    <location name="VRP" unit="IN">
66      <x> 101.65 </x>
67      <y>   0.0  </y>
68      <z>   0.0  </z>
69    </location>
70  </metrics>
71
72  <mass_balance>
73    <ixx unit="SLUG*FT2">    218368 </ixx>
74    <iyy unit="SLUG*FT2">    675849 </iyy>
75    <izz unit="SLUG*FT2">    860261 </izz>
76    <emptywt unit="LBS" >     51307 </emptywt>
77    <location name="CG" unit="IN">
78      <x> 719.81 </x> <!-- 693.81 -->
79      <y>   0.00 </y>
80      <z>  38.12 </z>
81    </location>
82    <pointmass name="pilot">
83      <weight unit="LBS"> 230 </weight>
84      <location name="POINTMASS" unit="IN">
85        <x> 122.04 </x>
86        <y> -30.0 </y>
87        <z>  66.0 </z>
88      </location>
89    </pointmass>
90    <pointmass name="copilot">
91      <weight unit="LBS"> 230 </weight>
92      <location name="POINTMASS" unit="IN">
93        <x> 122.04 </x>
94        <y>  30.0 </y>
95        <z>  66.0 </z>
96      </location>
97    </pointmass>
98    <pointmass name="steward">
99      <weight unit="LBS"> 400 </weight>
100      <location name="POINTMASS" unit="IN">
101        <x>  218 </x>
102        <y>  32.0 </y>
103        <z>  66.0 </z>
104      </location>
105    </pointmass>
106  </mass_balance>
107
108  <ground_reactions>
109
110   <contact type="BOGEY" name="NOSE">
111    <location unit="IN">
112      <x> 172.87 </x>
113      <y>   0.00 </y>
114      <z> -55.73 </z>
115    </location>
116    <static_friction>  0.80 </static_friction>
117    <dynamic_friction> 0.50 </dynamic_friction>
118    <rolling_friction> 0.02 </rolling_friction>
119    <spring_coeff unit="LBS/FT">       7750.03 </spring_coeff>
120    <damping_coeff unit="LBS/FT/SEC">  1600.34 </damping_coeff>
121    <max_steer unit="DEG"> 5.00 </max_steer>
122    <brake_group>NONE</brake_group>
123    <retractable>1</retractable>
124  </contact>
125
126   <contact type="BOGEY" name="LEFT_MAIN">
127    <location unit="IN">
128      <x> 731.93 </x>
129      <y>-101.65 </y>
130      <z> -63.53 </z>
131    </location>
132    <static_friction>  0.80 </static_friction>
133    <dynamic_friction> 0.50 </dynamic_friction>
134    <rolling_friction> 0.02 </rolling_friction>
135    <spring_coeff unit="LBS/FT">      95013.45 </spring_coeff>
136    <damping_coeff unit="LBS/FT/SEC"> 19002.69 </damping_coeff>
137    <max_steer unit="DEG">0</max_steer>
138    <brake_group>LEFT</brake_group>
139    <retractable>1</retractable>
140  </contact>
141
142   <contact type="BOGEY" name="RIGHT_MAIN">
143    <location unit="IN">
144      <x> 731.93 </x>
145      <y> 101.65 </y>
146      <z> -63.53 </z>
147    </location>
148    <static_friction>  0.80 </static_friction>
149    <dynamic_friction> 0.50 </dynamic_friction>
150    <rolling_friction> 0.02 </rolling_friction>
151    <spring_coeff unit="LBS/FT">      95013.45 </spring_coeff>
152    <damping_coeff unit="LBS/FT/SEC"> 19002.69 </damping_coeff>
153    <max_steer unit="DEG">0</max_steer>
154    <brake_group>RIGHT</brake_group>
155    <retractable>1</retractable>
156  </contact>
157
158   <contact type="STRUCTURE" name="LEFT_WING">
159     <location unit="IN">
160      <x> 753.77 </x>
161      <y>-1105.4 </y>
162      <z>   0.0 </z>
163     </location>
164     <static_friction>  0.80 </static_friction>
165     <dynamic_friction> 0.50 </dynamic_friction>
166     <spring_coeff unit="LBS/FT">      95013.45 </spring_coeff>
167     <damping_coeff unit="LBS/FT/SEC"> 19002.69 </damping_coeff>
168  </contact>
169
170   <contact type="STRUCTURE" name="RIGHT_WING">
171     <location unit="IN">
172      <x> 753.77 </x>
173      <y> 1105.4 </y>
174      <z>   0.0  </z>
175     </location>
176     <static_friction>  0.80 </static_friction>
177     <dynamic_friction> 0.50 </dynamic_friction>
178     <spring_coeff unit="LBS/FT">      95013.45 </spring_coeff>
179     <damping_coeff unit="LBS/FT/SEC"> 19002.69 </damping_coeff>
180  </contact>
181
182  </ground_reactions>
183
184  <external_reactions>
185     <force name="pushback" frame="BODY">
186        <location unit="IN">
187           <x>-139</x>
188           <y>0</y>
189           <z>-71</z>
190        </location>
191        <direction>
192           <x>1</x>
193           <y>0</y>
194           <z>0</z>
195        </direction>
196     </force>
197  </external_reactions>
198
199  <propulsion>
200
201    <engine file="PW1217G">
202     <location unit="IN">
203       <x>  922.52 </x>
204       <y> -101.65 </y>
205       <z>   43.53 </z>
206     </location>
207     <orient unit="DEG">
208       <pitch> 0.00 </pitch>
209       <roll>  0.00 </roll>
210       <yaw>   0.00 </yaw>
211     </orient>
212     <feed>0</feed>
213     <thruster file="direct">
214      <location unit="IN">
215        <x>  922.52 </x>
216        <y> -101.65 </y>
217        <z>   43.53 </z>
218      </location>
219      <orient unit="DEG">
220        <pitch> 0.00 </pitch>
221        <roll>  0.00 </roll>
222        <yaw>   0.00 </yaw>
223      </orient>
224     </thruster>
225   </engine>
226
227    <engine file="PW1217G">
228     <location unit="IN">
229       <x>  922.52 </x>
230       <y>  101.65 </y>
231       <z>   43.53 </z>
232     </location>
233     <orient unit="DEG">
234       <pitch> 0.00 </pitch>
235       <roll>  0.00 </roll>
236       <yaw>   0.00 </yaw>
237     </orient>
238     <feed>1</feed>
239     <thruster file="direct">
240      <location unit="IN">
241        <x>  922.52 </x>
242        <y>  101.65 </y>
243        <z>   43.53 </z>
244      </location>
245      <orient unit="DEG">
246        <pitch> 0.00 </pitch>
247        <roll>  0.00 </roll>
248        <yaw>   0.00 </yaw>
249      </orient>
250     </thruster>
251   </engine>
252
253   <tank type="FUEL" number="0">
254      <location unit="IN">
255        <x> 713.81 </x>
256        <y>-190.59 </y>
257        <z>   0.0  </z>
258      </location>
259      <capacity unit="LBS"> 13360.01 </capacity>
260      <contents unit="LBS">  8688.50 </contents>
261   </tank>
262
263   <tank type="FUEL" number="1">
264      <location unit="IN">
265        <x> 713.81 </x>
266        <y> 190.59 </y>
267        <z>   0.0  </z>
268      </location>
269      <capacity unit="LBS"> 13360.01 </capacity>
270      <contents unit="LBS">  8688.50 </contents>
271   </tank>
272   <tank type="FUEL" number="2">
273      <location unit="IN">
274        <x> 703.77 </x>
275        <y>   0.00 </y>
276        <z> -31.99 </z>
277      </location>
278      <capacity unit="LBS"> 1377.01 </capacity>
279      <contents unit="LBS"> 688.50 </contents>
280   </tank>
281  </propulsion>
282
283  <system file="pushback"/>
284
285  <flight_control name="FCS: Fokker-100">
286
287   <channel name="Pitch">
288    <summer name="fcs/pitch-trim-sum">
289       <input>fcs/elevator-cmd-norm</input>
290       <input>fcs/pitch-trim-cmd-norm</input>
291       <clipto>
292         <min> -1 </min>
293         <max>  1 </max>
294       </clipto>
295    </summer>
296
297    <aerosurface_scale name="fcs/elevator-control">
298       <input>fcs/pitch-trim-sum</input>
299       <range>
300         <min> -0.35 </min>
301         <max>  0.35 </max>
302       </range>
303       <output>fcs/elevator-pos-rad</output>
304    </aerosurface_scale>
305
306    <aerosurface_scale name="fcs/elevator-normalization">
307       <input>fcs/elevator-pos-rad</input>
308       <domain>
309         <min> -0.35 </min>
310         <max>  0.35 </max>
311       </domain>
312       <range>
313         <min> -1 </min>
314         <max>  1 </max>
315       </range>
316       <output>fcs/elevator-pos-norm</output>
317    </aerosurface_scale>
318
319   </channel>
320
321   <channel name="Roll">
322    <summer name="fcs/roll-trim-sum">
323       <input>fcs/aileron-cmd-norm</input>
324       <input>fcs/roll-trim-cmd-norm</input>
325       <clipto>
326         <min> -1 </min>
327         <max>  1 </max>
328       </clipto>
329    </summer>
330
331    <aerosurface_scale name="fcs/left-aileron-control">
332       <input>fcs/roll-trim-sum</input>
333       <range>
334         <min> -0.35 </min>
335         <max>  0.35 </max>
336       </range>
337       <output>fcs/left-aileron-pos-rad</output>
338    </aerosurface_scale>
339
340    <aerosurface_scale name="fcs/right-aileron-control">
341       <input>fcs/roll-trim-sum</input>
342       <range>
343         <min> -0.35 </min>
344         <max>  0.35 </max>
345       </range>
346       <output>fcs/right-aileron-pos-rad</output>
347    </aerosurface_scale>
348
349    <aerosurface_scale name="fcs/left-aileron-normalization">
350       <input>fcs/left-aileron-pos-rad</input>
351       <domain>
352         <min> -0.35 </min>
353         <max>  0.35 </max>
354       </domain>
355       <range>
356         <min> -1 </min>
357         <max>  1 </max>
358       </range>
359       <output>fcs/left-aileron-pos-norm</output>
360    </aerosurface_scale>
361
362    <aerosurface_scale name="fcs/right-aileron-normalization">
363       <input>fcs/right-aileron-pos-rad</input>
364       <domain>
365         <min> -0.35 </min>
366         <max>  0.35 </max>
367       </domain>
368       <range>
369         <min> -1 </min>
370         <max>  1 </max>
371       </range>
372       <output>fcs/right-aileron-pos-norm</output>
373    </aerosurface_scale>
374
375   </channel>
376
377   <channel name="Yaw">
378    <summer name="fcs/rudder-command-sum">
379       <input>fcs/rudder-cmd-norm</input>
380       <input>fcs/yaw-trim-cmd-norm</input>
381       <clipto>
382         <min> -0.35 </min>
383         <max>  0.35 </max>
384       </clipto>
385    </summer>
386
387    <scheduled_gain name="fcs/yaw-damper-rate">
388       <input>velocities/r-aero-rad_sec</input>
389       <table>
390         <independentVar lookup="row">velocities/ve-kts</independentVar>
391          <tableData>
392             30     0.00
393             60     2.00
394          </tableData>
395       </table>
396    </scheduled_gain>
397
398    <scheduled_gain name="fcs/yaw-damper-beta">
399       <input>aero/beta-rad</input>
400       <table>
401         <independentVar lookup="row">velocities/ve-kts</independentVar>
402         <tableData>
403            30     0.00
404            60     0.00
405         </tableData>
406       </table>
407    </scheduled_gain>
408
409    <summer name="fcs/yaw-damper-sum">
410       <input>fcs/yaw-damper-beta</input>
411       <input>fcs/yaw-damper-rate</input>
412       <clipto>
413         <min> -0.1 </min>
414         <max>  0.1 </max>
415       </clipto>
416    </summer>
417
418    <scheduled_gain name="fcs/yaw-damper-final">
419       <input>fcs/yaw-damper-sum</input>
420       <table>
421         <independentVar lookup="row">velocities/ve-kts</independentVar>
422         <tableData>
423            30         0.0
424            31         1.0
425         </tableData>
426       </table>
427    </scheduled_gain>
428
429    <summer name="fcs/rudder-sum">
430       <input>fcs/rudder-command-sum</input>
431       <input>fcs/yaw-damper-final</input>
432       <clipto>
433         <min> -1 </min>
434         <max>  1 </max>
435       </clipto>
436    </summer>
437
438    <aerosurface_scale name="fcs/rudder-control">
439       <input>fcs/rudder-sum</input>
440       <range>
441         <min> -0.35 </min>
442         <max>  0.35 </max>
443       </range>
444       <output>fcs/rudder-pos-rad</output>
445    </aerosurface_scale>
446
447    <aerosurface_scale name="rcs/rudder-normalization">
448       <input>fcs/rudder-pos-rad</input>
449       <domain>
450         <min> -0.35 </min>
451         <max>  0.35 </max>
452       </domain>
453       <range>
454         <min> -1 </min>
455         <max>  1 </max>
456       </range>
457       <output>fcs/rudder-pos-norm</output>
458    </aerosurface_scale>
459
460   </channel>
461
462   <channel name="Flaps">
463    <kinematic name="fcs/flaps-control">
464      <input>fcs/flap-cmd-norm</input>
465      <traverse>
466        <setting>
467          <position>0</position>
468          <time>0</time>
469        </setting>
470        <setting>
471          <position>8</position>
472          <time>3</time>
473        </setting>
474        <setting>
475          <position>15</position>
476          <time>3</time>
477        </setting>
478        <setting>
479          <position>25</position>
480          <time>4</time>
481        </setting>
482        <setting>
483          <position>42</position>
484          <time>4</time>
485        </setting>
486      </traverse>
487      <output>fcs/flap-pos-deg</output>
488    </kinematic>
489
490    <aerosurface_scale name="fcs/flap-normalization">
491       <input>fcs/flap-pos-deg</input>
492       <domain>
493         <min>0</min>
494         <max>42</max>
495       </domain>
496       <range>
497         <min>0</min>
498         <max>1</max>
499       </range>
500       <output>fcs/flap-pos-norm</output>
501    </aerosurface_scale>
502
503   </channel>
504
505   <channel name="Landing Gear">
506    <kinematic name="fcs/gear-control">
507      <input>gear/gear-cmd-norm</input>
508      <traverse>
509        <setting>
510           <position> 0 </position>
511           <time>     0 </time>
512        </setting>
513        <setting>
514           <position> 1 </position>
515           <time>     5 </time>
516        </setting>
517      </traverse>
518      <output>gear/gear-pos-norm</output>
519    </kinematic>
520
521   </channel>
522
523   <channel name="Speedbrake">
524    <kinematic name="fcs/speedbrake-control">
525      <input>fcs/speedbrake-cmd-norm</input>
526      <traverse>
527        <setting>
528           <position> 0 </position>
529           <time>     0 </time>
530        </setting>
531        <setting>
532           <position> 1 </position>
533           <time>     1 </time>
534        </setting>
535      </traverse>
536      <output>fcs/speedbrake-pos-norm</output>
537    </kinematic>
538   </channel>
539
540
541   <channel name="Spoilers">
542    <kinematic name="fcs/spoiler-control">
543      <input>fcs/spoiler-cmd-norm</input>
544      <traverse>
545         <setting>
546           <position>0</position>
547           <time>0</time>
548         </setting>
549         <setting>
550           <position>1</position>
551           <time>1</time>
552         </setting>
553      </traverse>
554      <output>fcs/spoiler-pos-norm</output>
555    </kinematic>
556   </channel>
557  </flight_control>
558
559     <aerodynamics>
560
561         <function name="aero/function/kCDge">
562             <description>Change_in_drag_due_to_ground_effect</description>
563             <product>
564                   <table>
565                       <independentVar>aero/h_b-mac-ft</independentVar>
566                       <tableData>
567                           0.0000        0.0350
568                           0.1000        0.4170
569                           0.1500        0.5390
570                           0.2000        0.6240
571                           0.3000        0.7510
572                           0.4000        0.8000
573                           0.5000        0.8960
574                           0.6000        0.9390
575                           0.7000        0.9740
576                           0.8000        0.9810
577                           0.9000        0.9900
578                           1.0000        0.9940
579                           1.1000        1.0000
580                       </tableData>
581                   </table>
582             </product>
583         </function>
584
585         <function name="aero/function/kCLge">
586             <description>Change_in_lift_due_to_ground_effect</description>
587             <product>
588                   <table>
589                       <independentVar>aero/h_b-mac-ft</independentVar>
590                       <tableData>
591                           0.0000        1.3910
592                           0.1000        1.2350
593                           0.1500        1.1670
594                           0.2000        1.1350
595                           0.3000        1.0850
596                           0.4000        1.1020
597                           0.5000        1.0350
598                           0.6000        1.0240
599                           0.7000        1.0150
600                           0.8000        1.0110
601                           0.9000        1.0060
602                           1.0000        1.0040
603                           1.1000        1.0000
604                       </tableData>
605                   </table>
606             </product>
607         </function>
608
609         <axis name="DRAG">
610             <function name="aero/coefficient/CD0">
611                 <description>Drag_at_zero_lift</description>
612                 <product>
613                     <property>aero/qbar-psf</property>
614                     <property>metrics/Sw-sqft</property>
615                     <property>aero/function/kCDge</property>
616                       <table>
617                           <independentVar>aero/alpha-rad</independentVar>
618                           <tableData>
619                               -1.5700   1.5000
620                               -0.2600   0.0392
621                               0.0000    0.01884
622                               0.2600    0.0392
623                               1.5700    1.4700
624                           </tableData>
625                       </table>
626                 </product>
627             </function>
628             <function name="aero/coefficient/CDi">
629                 <description>Induced_drag</description>
630                 <product>
631                     <property>aero/qbar-psf</property>
632                     <property>metrics/Sw-sqft</property>
633                     <property>aero/cl-squared</property>
634                     <property>aero/function/kCDge</property>
635                     <value>0.00717</value>
636                 </product>
637             </function>
638             <function name="aero/coefficient/CDflap">
639                 <description>Drag_due_to_flaps</description>
640                 <product>
641                     <property>aero/qbar-psf</property>
642                     <property>metrics/Sw-sqft</property>
643                     <property>fcs/flap-pos-norm</property>
644                     <property>aero/function/kCDge</property>
645                     <value>0.0830</value>
646                 </product>
647             </function>
648             <function name="aero/coefficient/CDmach">
649                 <description>Drag_due_to_mach</description>
650                 <product>
651                     <property>aero/qbar-psf</property>
652                     <property>metrics/Sw-sqft</property>
653                       <table>
654                           <independentVar>velocities/mach</independentVar>
655                           <tableData>
656                               0.0000    0.0000
657                               0.6500    0.0000
658                               0.7700    0.0015
659                               0.8600    0.0200
660                               1.1000    0.0390
661                               1.8000    0.0260
662                           </tableData>
663                       </table>
664                 </product>
665             </function>
666             <function name="aero/coefficient/CDgear">
667                 <description>Drag_due_to_gear</description>
668                 <product>
669                     <property>aero/qbar-psf</property>
670                     <property>metrics/Sw-sqft</property>
671                     <property>gear/gear-pos-norm</property>
672                     <value>0.0120</value>
673                 </product>
674             </function>
675             <function name="aero/coefficient/CDsb">
676                 <description>Drag_due_to_speedbrakes</description>
677                 <product>
678                     <property>aero/qbar-psf</property>
679                     <property>metrics/Sw-sqft</property>
680                     <property>fcs/speedbrake-pos-norm</property>
681                     <value>0.1200</value>
682                 </product>
683             </function>
684             <function name="aero/coefficient/CDsp">
685                 <description>Drag_due_to_spoilers</description>
686                 <product>
687                     <property>aero/qbar-psf</property>
688                     <property>metrics/Sw-sqft</property>
689                     <property>fcs/spoiler-pos-norm</property>
690                     <value>0.0280</value>
691                 </product>
692             </function>
693             <function name="aero/coefficient/CDrv">
694                 <description>Drag_due_to_reverse</description>
695                 <product>
696                     <property>aero/qbar-psf</property>
697                     <property>metrics/Sw-sqft</property>
698                     <property>propulsion/engine[0]/reverser-angle-rad</property>
699                     <property>propulsion/engine[1]/reverser-angle-rad</property>
700                     <value>0.0187</value>
701                 </product>
702             </function>
703             <function name="aero/coefficient/CDbeta">
704                 <description>Drag_due_to_sideslip</description>
705                 <product>
706                     <property>aero/qbar-psf</property>
707                     <property>metrics/Sw-sqft</property>
708                       <table>
709                           <independentVar>aero/beta-rad</independentVar>
710                           <tableData>
711                               -1.5700   1.2300
712                               -0.2600   0.0500
713                               0.0000    0.0000
714                               0.2600    0.0500
715                               1.5700    1.2300
716                           </tableData>
717                       </table>
718                 </product>
719             </function>
720             <function name="aero/coefficient/CDde">
721                 <description>Drag_due_to_Elevator_Deflection</description>
722                 <product>
723                     <property>aero/qbar-psf</property>
724                     <property>metrics/Sw-sqft</property>
725                     <property>fcs/mag-elevator-pos-rad</property>
726                     <value>0.0590</value>
727                 </product>
728             </function>
729         </axis>
730
731         <axis name="SIDE">
732             <function name="aero/coefficient/CYb">
733                 <description>Side_force_due_to_beta</description>
734                 <product>
735                     <property>aero/qbar-psf</property>
736                     <property>metrics/Sw-sqft</property>
737                     <property>aero/beta-rad</property>
738                     <value>-1.0000</value>
739                 </product>
740             </function>
741         </axis>
742
743         <axis name="LIFT">
744             <function name="aero/coefficient/CLalpha">
745                 <description>Lift_due_to_alpha</description>
746                 <product>
747                     <property>aero/qbar-psf</property>
748                     <property>metrics/Sw-sqft</property>
749                     <property>aero/function/kCLge</property>
750                       <table>
751                           <independentVar>aero/alpha-rad</independentVar>
752                           <tableData>
753                               -0.20 -0.680
754                                0.00  0.221
755                                0.23  1.300
756                                0.60  0.612
757                           </tableData>
758                       </table>
759                 </product>
760             </function>
761             <function name="aero/coefficient/dCLflap">
762                 <description>Delta_Lift_due_to_flaps</description>
763                 <product>
764                     <property>aero/qbar-psf</property>
765                     <property>metrics/Sw-sqft</property>
766                     <property>aero/function/kCLge</property>
767                       <table>
768                           <independentVar>fcs/flap-pos-norm</independentVar>
769                           <tableData>
770                               0.0000    0.0000
771                               0.3570    0.4900
772                               1.0000    1.1800
773                           </tableData>
774                       </table>
775                 </product>
776             </function>
777             <function name="aero/coefficient/dCLsp">
778                 <description>Delta_Lift_due_to_spoiler</description>
779                 <product>
780                     <property>aero/qbar-psf</property>
781                     <property>metrics/Sw-sqft</property>
782                     <property>fcs/spoiler-pos-norm</property>
783                     <property>aero/function/kCLge</property>
784                     <value>-0.1200</value>
785                 </product>
786             </function>
787             <function name="aero/coefficient/CLde">
788                 <description>Lift_due_to_Elevator_Deflection</description>
789                 <product>
790                     <property>aero/qbar-psf</property>
791                     <property>metrics/Sw-sqft</property>
792                     <property>fcs/elevator-pos-rad</property>
793                     <value>0.2000</value>
794                 </product>
795             </function>
796         </axis>
797
798         <axis name="ROLL">
799             <function name="aero/coefficient/Clb">
800                 <description>Roll_moment_due_to_beta</description>
801                 <product>
802                     <property>aero/qbar-psf</property>
803                     <property>metrics/Sw-sqft</property>
804                     <property>metrics/bw-ft</property>
805                     <property>aero/beta-rad</property>
806                     <value>-0.1000</value>
807                 </product>
808             </function>
809             <function name="aero/coefficient/Clp">
810                 <description>Roll_moment_due_to_roll_rate</description>
811                 <product>
812                     <property>aero/qbar-psf</property>
813                     <property>metrics/Sw-sqft</property>
814                     <property>metrics/bw-ft</property>
815                     <property>aero/bi2vel</property>
816                     <property>velocities/p-aero-rad_sec</property>
817                     <value>-0.4000</value>
818                 </product>
819             </function>
820             <function name="aero/coefficient/Clr">
821                 <description>Roll_moment_due_to_yaw_rate</description>
822                 <product>
823                     <property>aero/qbar-psf</property>
824                     <property>metrics/Sw-sqft</property>
825                     <property>metrics/bw-ft</property>
826                     <property>aero/bi2vel</property>
827                     <property>velocities/r-aero-rad_sec</property>
828                     <value>0.1500</value>
829                 </product>
830             </function>
831             <function name="aero/coefficient/Clda">
832                 <description>Roll_moment_due_to_aileron</description>
833                 <product>
834                     <property>aero/qbar-psf</property>
835                     <property>metrics/Sw-sqft</property>
836                     <property>metrics/bw-ft</property>
837                     <property>fcs/left-aileron-pos-rad</property>
838                       <table>
839                           <independentVar>velocities/mach</independentVar>
840                           <tableData>
841                               0.0000    0.1000
842                               2.0000    0.0330
843                           </tableData>
844                       </table>
845                 </product>
846             </function>
847             <function name="aero/coefficient/Cldr">
848                 <description>Roll_moment_due_to_rudder</description>
849                 <product>
850                     <property>aero/qbar-psf</property>
851                     <property>metrics/Sw-sqft</property>
852                     <property>metrics/bw-ft</property>
853                     <property>fcs/rudder-pos-rad</property>
854                     <value>0.0100</value>
855                 </product>
856             </function>
857         </axis>
858
859         <axis name="PITCH">
860             <function name="aero/function/kCmge">
861                 <description>Change_in_lift_due_to_ground_effect</description>
862                 <product>
863                       <table>
864                           <independentVar>aero/h_b-mac-ft</independentVar>
865                           <tableData>
866                               0.0000    1.2030
867                               0.1000    1.1270
868                               0.1500    1.0900
869                               0.2000    1.0730
870                               0.3000    1.0460
871                               0.4000    1.0550
872                               0.5000    1.0190
873                               0.6000    1.0130
874                               0.7000    1.0080
875                               0.8000    1.0060
876                               0.9000    1.0030
877                               1.0000    1.0020
878                               1.1000    1.0000
879                           </tableData>
880                       </table>
881                 </product>
882             </function>
883
884             <function name="aero/coefficient/Cmo">
885                 <description>Pitching_moment_at_zero_alpha</description>
886                 <product>
887                     <property>aero/qbar-psf</property>
888                     <property>metrics/Sw-sqft</property>
889                     <property>metrics/cbarw-ft</property>
890                     <property>aero/function/kCmge</property>
891                     <value>-0.000737</value>
892                 </product>
893             </function>
894             <function name="aero/coefficient/Cmalpha">
895                 <description>Pitch_moment_due_to_alpha</description>
896                 <product>
897                     <property>aero/qbar-psf</property>
898                     <property>metrics/Sw-sqft</property>
899                     <property>metrics/cbarw-ft</property>
900                     <property>aero/alpha-rad</property>
901                     <value>-0.6000</value>
902                 </product>
903             </function>
904             <function name="aero/coefficient/Cmde">
905                 <description>Pitch_moment_due_to_elevator</description>
906                 <product>
907                     <property>aero/qbar-psf</property>
908                     <property>metrics/Sw-sqft</property>
909                     <property>metrics/cbarw-ft</property>
910                     <property>fcs/elevator-pos-rad</property>
911                       <table>
912                           <independentVar>velocities/mach</independentVar>
913                           <tableData>
914                               0.0000    -1.2000
915                               2.0000    -0.3000
916                           </tableData>
917                       </table>
918                 </product>
919             </function>
920             <function name="aero/coefficient/Cmq">
921                 <description>Pitch_moment_due_to_pitch_rate</description>
922                 <product>
923                     <property>aero/qbar-psf</property>
924                     <property>metrics/Sw-sqft</property>
925                     <property>metrics/cbarw-ft</property>
926                     <property>aero/ci2vel</property>
927                     <property>velocities/q-aero-rad_sec</property>
928                     <value>-31.0000</value>
929                 </product>
930             </function>
931             <function name="aero/coefficient/Cmadot">
932                 <description>Pitch_moment_due_to_alpha_rate</description>
933                 <product>
934                     <property>aero/qbar-psf</property>
935                     <property>metrics/Sw-sqft</property>
936                     <property>metrics/cbarw-ft</property>
937                     <property>aero/ci2vel</property>
938                     <property>aero/alphadot-rad_sec</property>
939                     <value>-16.0000</value>
940                 </product>
941             </function>
942         </axis>
943
944         <axis name="YAW">
945             <function name="aero/coefficient/Cnb">
946                 <description>Yaw_moment_due_to_beta</description>
947                 <product>
948                     <property>aero/qbar-psf</property>
949                     <property>metrics/Sw-sqft</property>
950                     <property>metrics/bw-ft</property>
951                     <property>aero/beta-rad</property>
952                     <value>0.1200</value>
953                 </product>
954             </function>
955             <function name="aero/coefficient/Cnr">
956                 <description>Yaw_moment_due_to_yaw_rate</description>
957                 <product>
958                     <property>aero/qbar-psf</property>
959                     <property>metrics/Sw-sqft</property>
960                     <property>metrics/bw-ft</property>
961                     <property>aero/bi2vel</property>
962                     <property>velocities/r-aero-rad_sec</property>
963                     <value>-0.1500</value>
964                 </product>
965             </function>
966             <function name="aero/coefficient/Cndr">
967                 <description>Yaw_moment_due_to_rudder</description>
968                 <product>
969                     <property>aero/qbar-psf</property>
970                     <property>metrics/Sw-sqft</property>
971                     <property>metrics/bw-ft</property>
972                     <property>fcs/rudder-pos-rad</property>
973                     <value>-0.1000</value>
974                 </product>
975             </function>
976             <function name="aero/coefficient/Cnda">
977                 <description>Adverse_yaw</description>
978                 <product>
979                     <property>aero/qbar-psf</property>
980                     <property>metrics/Sw-sqft</property>
981                     <property>metrics/bw-ft</property>
982                     <property>fcs/left-aileron-pos-rad</property>
983                     <value>0.0000</value>
984                 </product>
985             </function>
986         </axis>
987     </aerodynamics>
988 </fdm_config>